[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 20th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
143/12:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 210
6
145/00:25:31
981 -2
4 3
4 3
4
N/A -0
6 -0
1 220
2
000/00:06:59
963 -2
2 -0
0 212
1
Coasting Arc #1 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2012/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3515129
63 A = 6775135
14 meter
Y = 3803809
04 meter E =
0013070
Z = -4377789
70 I = 51
28166
XDOT = -2679
279825 Wp = 12
80229
YDOT = -6347
844170 meter/sec RA = 270
08365 deg
ZDOT = -3353
651355 TA = 223
02722
MA = 223
12949
Ha = 219
240 n
mi
Hp = 211
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11532577
53 X = -3536136
64
Y = 12479688
46 feet Y = 3764383
48 meter
Z = -14362827
11 Z = -4394917
17
XDOT = -8790
288141 XDOT = -2591
806225
YDOT = -20826
260400 feet/sec YDOT = -6377
316251 meter/sec
ZDOT = -11002
793160 ZDOT = -3366
455306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3880225
54 X = 1182692
74
Y = 16481819
43 feet Y = 5023658
56 meter
Z = -14433545
96 Z = -4399344
81
XDOT = -20924
703343 XDOT = -6377
849579
YDOT = -4785
093245 feet/sec YDOT = -1458
496421 meter/sec
ZDOT = -11054
820859 ZDOT = -3369
509398
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12139
52214332
00016717 00000-0 10270-3 0 9005
2 25544 51
6381 270
7450 0011066 330
0522 29
9998 15
56189716 13391
Satellite: ISS
Catalog Number: 25544
Epoch time: 12139
52214332 = yrday
fracday
Element set: 900
Inclination: 51
6381 deg
RA of node: 270
7450 deg
Eccentricity:
0011066
Arg of perigee: 330
0522 deg
Mean anomaly: 29
9998 deg
Mean motion: 15
56189716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 300
Coasting Arc #2 (Orbit 1354)
---------------------------------------
Vector Time (GMT): 2012/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4100909
23 A = 6771417
40 meter
Y = -1287256
06 meter E =
0008651
Z = 5233179
81 I = 51
27151
XDOT = 1316
150347 Wp = 345
88019
YDOT = 7512
727988 meter/sec RA = 265
04046 deg
ZDOT = 825
134225 TA = 96
24438
MA = 96
14583
Ha = 219
253 n
mi
Hp = 211
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13454426
62 X = 4089576
72
Y = -4223281
03 feet Y = -1241460
91 meter
Z = 17169225
11 Z = 5253074
60
XDOT = 4318
078567 XDOT = 1228
035282
YDOT = 24648
057703 feet/sec YDOT = 7526
953255 meter/sec
ZDOT = 2707
133283 ZDOT = 831
314675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3786499
24 X = 1154124
97
Y = -13479703
48 feet Y = -4108613
62 meter
Z = 17251087
12 Z = 5258131
35
XDOT = 21990
010093 XDOT = 6702
555076
YDOT = 9637
561432 feet/sec YDOT = 2937
528724 meter/sec
ZDOT = 2731
844729 ZDOT = 832
666273
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12140
54960088
00016717 00000-0 10270-3 0 9016
2 25544 51
6388 265
6057 0011174 333
7981 26
2606 15
56245266 13550
Satellite: ISS
Catalog Number: 25544
Epoch time: 12140
54960088 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 265
6057 deg
Eccentricity:
0011174
Arg of perigee: 333
7981 deg
Mean anomaly: 26
2606 deg
Mean motion: 15
56245266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1355
Checksum: 310
Coasting Arc #3 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2012/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4333528
51 A = 6772272
77 meter
Y = -1373490
82 meter E =
0011156
Z = -5025112
72 I = 51
27850
XDOT = 206
020448 Wp = 50
01357
YDOT = -7434
443857 meter/sec RA = 259
99411 deg
ZDOT = 1864
152544 TA = 238
08930
MA = 238
19787
Ha = 219
405 n
mi
Hp = 211
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14217613
21 X = -4293436
47
Y = -4506203
49 feet Y = -1421726
39 meter
Z = -16486590
28 Z = -5046067
93
XDOT = 675
920104 XDOT = 280
082805
YDOT = -24391
220002 feet/sec YDOT = -7431
726074 meter/sec
ZDOT = 6115
986038 ZDOT = 1865
332618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11345861
88 X = -3458218
70
Y = 9532853
33 feet Y = 2905613
69 meter
Z = -16572573
12 Z = -5051320
29
XDOT = -19590
711380 XDOT = -5971
248829
YDOT = -12730
112180 feet/sec YDOT = -3880
138193 meter/sec
ZDOT = 6121
507996 ZDOT = 1865
835637
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12141
51282773
00016717 00000-0 10270-3 0 9023
2 25544 51
6390 260
7896 0011141 338
0397 22
0278 15
56267769 13701
Satellite: ISS
Catalog Number: 25544
Epoch time: 12141
51282773 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 260
7896 deg
Eccentricity:
0011141
Arg of perigee: 338
0397 deg
Mean anomaly: 22
0278 deg
Mean motion: 15
56267769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1370
Checksum: 308
Coasting Arc #4 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2012/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147977
13 A = 6777078
96 meter
Y = 3819412
69 meter E =
0014397
Z = 3762968
29 I = 51
30096
XDOT = -1832
216325 Wp = 33
79251
YDOT = 6147
084234 meter/sec RA = 254
95791 deg
ZDOT = -4200
076260 TA = 100
86963
MA = 100
70757
Ha = 219
660 n
mi
Hp = 210
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13608848
84 X = 4086679
45
Y = 12530881
51 feet Y = 3865454
80 meter
Z = 12345696
48 Z = 3782970
81
XDOT = -6011
208416 XDOT = -1880
414749
YDOT = 20167
599194 feet/sec YDOT = 6126
326211 meter/sec
ZDOT = -13779
777755 ZDOT = -4209
093651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17736017
16 X = 5405938
03
Y = -5062572
65 feet Y = -1543072
14 meter
Z = 12427551
39 Z = 3787917
66
XDOT = 13791
298480 XDOT = 4203
587777
YDOT = 14240
823314 feet/sec YDOT = 4340
602946 meter/sec
ZDOT = -13817
387101 ZDOT = -4211
539589
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12142
54025259
00016717 00000-0 10270-3 0 9032
2 25544 51
6393 255
6505 0011135 342
0853 17
9907 15
56249986 13869
Satellite: ISS
Catalog Number: 25544
Epoch time: 12142
54025259 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 255
6505 deg
Eccentricity:
0011135
Arg of perigee: 342
0853 deg
Mean anomaly: 17
9907 deg
Mean motion: 15
56249986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1386
Checksum: 315
Coasting Arc #5 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2012/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3499415
59 A = 6781790
30 meter
Y = -5530566
82 meter E =
0017068
Z = -1737165
66 I = 51
32628
XDOT = 3394
344574 Wp = 6
13742
YDOT = -3919
697773 meter/sec RA = 249
94279 deg
ZDOT = 5663
146763 TA = 334
67847
MA = 334
76202
Ha = 219
812 n
mi
Hp = 210
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11481022
27 X = -3428872
71
Y = -18144904
26 feet Y = -5569304
82 meter
Z = -5699362
39 Z = -1753995
18
XDOT = 11136
301097 XDOT = 3410
412508
YDOT = -12859
900830 feet/sec YDOT = -3881
650929 meter/sec
ZDOT = 18579
877830 ZDOT = 5679
675129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21441218
90 X = -6535283
52
Y = 733533
03 feet Y = 223580
87 meter
Z = -5768034
00 Z = -1758096
76
XDOT = -5491
633123 XDOT = -1673
849776
YDOT = -14439
731556 feet/sec YDOT = -4401
230178 meter/sec
ZDOT = 18648
155731 ZDOT = 5683
957867
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12143
50344569
00016717 00000-0 10270-3 0 9048
2 25544 51
6398 250
8331 0011458 345
5554 14
5271 15
56272218 14011
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
50344569 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 250
8331 deg
Eccentricity:
0011458
Arg of perigee: 345
5554 deg
Mean anomaly: 14
5271 deg
Mean motion: 15
56272218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1401
Checksum: 293
Coasting Arc #6 (Orbit 1401)
---------------------------------------
Vector Time (GMT): 2012/143/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945769
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4257288
32 A = 6771162
18 meter
Y = -576928
69 meter E =
0012600
Z = 5235175
61 I = 51
29169
XDOT = 2008
943579 Wp = 359
93248
YDOT = 7358
984760 meter/sec RA = 249
84733 deg
ZDOT = -810
325052 TA = 97
91888
MA = 97
77585
Ha = 219
680 n
mi
Hp = 210
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13967481
36 X = 4237991
61
Y = -1892810
66 feet Y = -529429
56 meter
Z = 17175773
00 Z = 5255810
66
XDOT = 6591
022240 XDOT = 1930
441030
YDOT = 24143
650787 feet/sec YDOT = 7381
011172 meter/sec
ZDOT = -2658
546758 ZDOT = -800
755393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3619566
93 X = 1103244
00
Y = -13514800
33 feet Y = -4119311
14 meter
Z = 17260630
15 Z = 5261040
07
XDOT = 23833
875564 XDOT = 7264
565272
YDOT = 2985
585741 feet/sec YDOT = 910
006534 meter/sec
ZDOT = -2619
874664 ZDOT = -798
537798
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12143
56765704
00016717 00000-0 10270-3 0 9053
2 25544 51
6400 250
5119 0011397 345
5643 14
5183 15
56329928 14021
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
56765704 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 250
5119 deg
Eccentricity:
0011397
Arg of perigee: 345
5643 deg
Mean anomaly: 14
5183 deg
Mean motion: 15
56329928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1402
Checksum: 298
Coasting Arc #7 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2012/144/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945769
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4789825
79 A = 6774613
23 meter
Y = -1940213
22 meter E =
0010258
Z = -4381401
09 I = 51
31451
XDOT = -269
639639 Wp = 39
08326
YDOT = -6890
361106 meter/sec RA = 244
80727 deg
ZDOT = 3358
150361 TA = 264
97662
MA = 265
09373
Ha = 219
792 n
mi
Hp = 210
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15714651
53 X = -4746489
87
Y = -6365528
92 feet Y = -1993533
18 meter
Z = -14374675
49 Z = -4404565
05
XDOT = -884
644486 XDOT = -208
883472
YDOT = -22606
171606 feet/sec YDOT = -6893
037079 meter/sec
ZDOT = 11017
553679 ZDOT = 3356
987201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11709851
90 X = -3569162
86
Y = 12149416
64 feet Y = 3703142
19 meter
Z = -14469712
18 Z = -4410368
27
XDOT = -20459
196919 XDOT = -6235
963221
YDOT = -6649
318249 feet/sec YDOT = -2026
712202 meter/sec
ZDOT = 11013
382029 ZDOT = 3356
878843
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12144
53083577
00016717 00000-0 10270-3 0 9063
2 25544 51
6396 245
6955 0011374 349
5023 10
5892 15
56346431 14176
Satellite: ISS
Catalog Number: 25544
Epoch time: 12144
53083577 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 245
6955 deg
Eccentricity:
0011374
Arg of perigee: 349
5023 deg
Mean anomaly: 10
5892 deg
Mean motion: 15
56346431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1417
Checksum: 313
Coasting Arc #8 (Orbit 1424)
---------------------------------------
Vector Time (GMT): 2012/145/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -314510
93 A = 6779060
41 meter
Y = 5706739
98 meter E =
0010690
Z = -3657213
44 I = 51
32919
XDOT = -5521
845397 Wp = 13
94812
YDOT = -3080
947341 meter/sec RA = 242
34992 deg
ZDOT = -4325
129075 TA = 209
70935
MA = 209
77010
Ha = 220
185 n
mi
Hp = 212
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1031860
00 X = -360535
42
Y = 18722900
21 feet Y = 5702966
03 meter
Z = -11998731
75 Z = -3658852
44
XDOT = -18116
290672 XDOT = -5465
972549
YDOT = -10108
094951 feet/sec YDOT = -3142
383115 meter/sec
ZDOT = -14190
056021 ZDOT = -4351
818825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17064231
53 X = -5201177
77
Y = -7762085
41 feet Y = -2365883
63 meter
Z = -12005970
32 Z = -3659419
75
XDOT = 15453
799569 XDOT = 4710
318109
YDOT = -11817
861732 feet/sec YDOT = -3602
084256 meter/sec
ZDOT = -14299
490631 ZDOT = -4358
484744
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12145
04453376
00016717 00000-0 10270-3 0 9079
2 25544 51
6391 243
1278 0009902 342
8871 17
1947 15
55709570 14252
Satellite: ISS
Catalog Number: 25544
Epoch time: 12145
04453376 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 243
1278 deg
Eccentricity:
0009902
Arg of perigee: 342
8871 deg
Mean anomaly: 17
1947 deg
Mean motion: 15
55709570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1425
Checksum: 315
Coasting Arc #9 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2012/146/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1938619
30 A = 6774392
68 meter
Y = -4247050
88 meter E =
0006945
Z = 4903861
21 I = 51
32820
XDOT = 5352
151746 Wp = 28
10392
YDOT = 5023
883276 meter/sec RA = 237
32323 deg
ZDOT = 2239
882600 TA = 39
97064
MA = 39
91953
Ha = 220
199 n
mi
Hp = 211
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6360299
55 X = 1962144
64
Y = -13933893
96 feet Y = -4225241
05 meter
Z = 16088783
50 Z = 4913335
65
XDOT = 17559
552974 XDOT = 5284
694976
YDOT = 16482
556681 feet/sec YDOT = 5083
356925 meter/sec
ZDOT = 7348
696193 ZDOT = 2265
719959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10849521
50 X = 3306934
15
Y = 10753048
59 feet Y = 3277529
21 meter
Z = 16128099
55 Z = 4915844
74
XDOT = -20796
625722 XDOT = -6338
811520
YDOT = 9825
711471 feet/sec YDOT = 2994
876856 meter/sec
ZDOT = 7454
473265 ZDOT = 2272
123451
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12146
07232069
00016717 00000-0 10270-3 0 9088
2 25544 51
6385 237
9911 0009892 346
5414 13
5474 15
55728440 14412
Satellite: ISS
Catalog Number: 25544
Epoch time: 12146
07232069 = yrday
fracday
Element set: 908
Inclination: 51
6385 deg
RA of node: 237
9911 deg
Eccentricity:
0009892
Arg of perigee: 346
5414 deg
Mean anomaly: 13
5474 deg
Mean motion: 15
55728440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 314
Coasting Arc #10 (Orbit 1455)
---------------------------------------
Vector Time (GMT): 2012/147/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3514167
29 A = 6772624
67 meter
Y = 2375083
31 meter E =
0016173
Z = -5291071
31 I = 51
34022
XDOT = -4528
050947 Wp = 54
59265
YDOT = -6175
851644 meter/sec RA = 232
28582 deg
ZDOT = 244
868250 TA = 217
69627
MA = 217
80970
Ha = 220
358 n
mi
Hp = 211
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11529420
23 X = -3514761
86
Y = 7792268
09 feet Y = 2335782
92 meter
Z = -17359157
84 Z = -5308144
23
XDOT = -14855
810192 XDOT = -4459
844297
YDOT = -20261
980460 feet/sec YDOT = -6226
105772 meter/sec
ZDOT = 803
373522 ZDOT = 223
036170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3517797
68 X = -1072224
73
Y = -13372477
93 feet Y = -4075931
27 meter
Z = -17429551
54 Z = -5312527
31
XDOT = 23092
286043 XDOT = 7038
528786
YDOT = -6964
110271 feet/sec YDOT = -2122
660810 meter/sec
ZDOT = 714
144225 ZDOT = 217
671160
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12147
03585634
00016717 00000-0 10270-3 0 9095
2 25544 51
6388 233
1757 0010012 350
1467 9
9489 15
55759911 14564
Satellite: ISS
Catalog Number: 25544
Epoch time: 12147
03585634 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 233
1757 deg
Eccentricity:
0010012
Arg of perigee: 350
1467 deg
Mean anomaly: 9
9489 deg
Mean motion: 15
55759911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1456
Checksum: 323
Coasting Arc #11 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2012/148/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4857367
25 A = 6774907
84 meter
Y = -296325
33 meter E =
0014772
Z = 4714626
30 I = 51
36738
XDOT = 3047
256880 Wp = 22
65629
YDOT = 6493
380580 meter/sec RA = 227
25025 deg
ZDOT = -2715
155375 TA = 94
37680
MA = 94
20800
Ha = 220
414 n
mi
Hp = 211
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15936244
24 X = 4837417
16
Y = -972195
96 feet Y = -242119
19 meter
Z = 15467934
05 Z = 4738174
74
XDOT = 9997
561943 XDOT = 2987
609737
YDOT = 21303
742060 feet/sec YDOT = 6527
123618 meter/sec
ZDOT = -8907
990076 ZDOT = -2700
496232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4124666
22 X = -1257198
26
Y = 15326145
64 feet Y = 4671409
19 meter
Z = 15564781
33 Z = 4744145
35
XDOT = -22277
573599 XDOT = -6790
204433
YDOT = 3044
320552 feet/sec YDOT = 927
908904 meter/sec
ZDOT = -8848
263179 ZDOT = -2696
950617
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12148
06361136
00016717 00000-0 10270-3 0 9100
2 25544 51
6384 228
0388 0010153 353
4888 6
6132 15
55801903 14728
Satellite: ISS
Catalog Number: 25544
Epoch time: 12148
06361136 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 228
0388 deg
Eccentricity:
0010153
Arg of perigee: 353
4888 deg
Mean anomaly: 6
6132 deg
Mean motion: 15
55801903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 292
Coasting Arc #12 (Orbit 1486)
---------------------------------------
Vector Time (GMT): 2012/149/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5692136
84 A = 6779732
95 meter
Y = -1598322
23 meter E =
0011224
Z = -3310529
74 I = 51
40521
XDOT = -1033
966631 Wp = 22
30035
YDOT = -5987
395203 meter/sec RA = 222
23019 deg
ZDOT = 4683
923303 TA = 299
01008
MA = 299
12252
Ha = 220
527 n
mi
Hp = 211
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18674989
62 X = -5657759
16
Y = -5243839
34 feet Y = -1661782
78 meter
Z = -10861318
03 Z = -3338098
59
XDOT = -3392
278972 XDOT = -989
691029
YDOT = -19643
685050 feet/sec YDOT = -5998
710432 meter/sec
ZDOT = 15367
202437 ZDOT = 4679
007441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10621608
96 X = 3237466
41
Y = -16154319
36 feet Y = -4923836
54 meter
Z = -10974548
13 Z = -3345042
27
XDOT = 18599
936212 XDOT = 5669
260557
YDOT = 1837
187323 feet/sec YDOT = 559
974696 meter/sec
ZDOT = 15347
484583 ZDOT = 4677
913301
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12149
02711859
00016717 00000-0 10270-3 0 9119
2 25544 51
6387 223
2227 0010183 356
9430 3
1659 15
55792833 14877
Satellite: ISS
Catalog Number: 25544
Epoch time: 12149
02711859 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 223
2227 deg
Eccentricity:
0010183
Arg of perigee: 356
9430 deg
Mean anomaly: 3
1659 deg
Mean motion: 15
55792833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1487
Checksum: 310
Coasting Arc #13 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2012/150/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5855340
75 A = 6783795
86 meter
Y = 3183895
15 meter E =
0012440
Z = 1263861
43 I = 51
44178
XDOT = -1345
052652 Wp = 76
31398
YDOT = 4804
113129 meter/sec RA = 217
22916 deg
ZDOT = -5819
752512 TA = 89
90267
MA = 89
76011
Ha = 220
735 n
mi
Hp = 210
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19210435
52 X = 5813163
01
Y = 10445850
23 feet Y = 3249137
29 meter
Z = 4146527
00 Z = 1292204
33
XDOT = -4412
902400 XDOT = -1370
402038
YDOT = 15761
526014 feet/sec YDOT = 4788
930535 meter/sec
ZDOT = -19093
676221 ZDOT = -5826
348040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15491616
89 X = -4721844
83
Y = 15400924
32 feet Y = 4694201
73 meter
Z = 4262820
92 Z = 1299307
82
XDOT = -12752
969914 XDOT = -3887
105230
YDOT = -7490
302798 feet/sec YDOT = -2283
044293 meter/sec
ZDOT = -19121
192286 ZDOT = -5828
139409
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12150
05484499
00016717 00000-0 10270-3 0 9122
2 25544 51
6387 218
0857 0010058 1
2756 358
8421 15
55786086 15039
Satellite: ISS
Catalog Number: 25544
Epoch time: 12150
05484499 = yrday
fracday
Element set: 912
Inclination: 51
6387 deg
RA of node: 218
0857 deg
Eccentricity:
0010058
Arg of perigee: 1
2756 deg
Mean anomaly: 358
8421 deg
Mean motion: 15
55786086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 315
Coasting Arc #14 (Orbit 1518)
---------------------------------------
Vector Time (GMT): 2012/151/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5208493
44 A = 6783963
49 meter
Y = -4212080
73 meter E =
0021489
Z = 985005
29 I = 51
46768
XDOT = 3720
869124 Wp = 33
75883
YDOT = -3210
445839 meter/sec RA = 212
23734 deg
ZDOT = 5902
321188 TA = 336
95943
MA = 337
05566
Ha = 220
782 n
mi
Hp = 210
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17088233
06 X = -5165790
96
Y = -13819162
50 feet Y = -4270086
62 meter
Z = 3231644
66 Z = 959805
89
XDOT = 12207
575866 XDOT = 3727
820007
YDOT = -10532
958788 feet/sec YDOT = -3168
798253 meter/sec
ZDOT = 19364
570827 ZDOT = 5920
413883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17913677
67 X = 5460088
95
Y = -12756725
95 feet Y = -3888250
07 meter
Z = 3128351
60 Z = 953521
57
XDOT = 5958
844212 XDOT = 1816
255716
YDOT = 13171
672164 feet/sec YDOT = 4014
725676 meter/sec
ZDOT = 19439
239841 ZDOT = 5925
080303
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12151
08255331
00016717 00000-0 10270-3 0 9138
2 25544 51
6387 212
9480 0010267 4
1765 355
9472 15
55846648 15190
Satellite: ISS
Catalog Number: 25544
Epoch time: 12151
08255331 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 212
9480 deg
Eccentricity:
0010267
Arg of perigee: 4
1765 deg
Mean anomaly: 355
9472 deg
Mean motion: 15
55846648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1519
Checksum: 312
Coasting Arc #15 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2012/152/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3778507
19 A = 6780354
34 meter
Y = 4714377
62 meter E =
0010413
Z = -3092959
55 I = 51
48143
XDOT = -5741
290139 Wp = 32
66897
YDOT = 1405
120008 meter/sec RA = 207
24164 deg
ZDOT = -4871
207844 TA = 182
95213
MA = 182
95828
Ha = 220
875 n
mi
Hp = 210
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12396677
13 X = 3740534
34
Y = 15467118
17 feet Y = 4756419
11 meter
Z = -10147505
10 Z = -3074695
40
XDOT = -18836
253737 XDOT = -5732
912206
YDOT = 4609
973780 feet/sec YDOT = 1340
964509 meter/sec
ZDOT = -15981
653033 ZDOT = -4899
078728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18111493
93 X = -5520383
35
Y = 8148271
91 feet Y = 2483593
28 meter
Z = -10072768
27 Z = -3070179
77
XDOT = 867
133880 XDOT = 264
302407
YDOT = -17974
392479 feet/sec YDOT = -5478
594828 meter/sec
ZDOT = -16096
397912 ZDOT = -4906
182084
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12152
04601769
00016717 00000-0 10270-3 0 9146
2 25544 51
6383 208
1321 0010204 7
1244 353
0053 15
55841773 15348
Satellite: ISS
Catalog Number: 25544
Epoch time: 12152
04601769 = yrday
fracday
Element set: 914
Inclination: 51
6383 deg
RA of node: 208
1321 deg
Eccentricity:
0010204
Arg of perigee: 7
1244 deg
Mean anomaly: 353
0053 deg
Mean motion: 15
55841773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 268
Coasting Arc #16 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2012/153/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1695825
17 A = 6775286
03 meter
Y = -4655296
53 meter E =
0011832
Z = 4609627
04 I = 51
49194
XDOT = 7077
893254 Wp = 56
01796
YDOT = 349
912729 meter/sec RA = 202
22974 deg
ZDOT = 2958
293769 TA = 4
49561
MA = 4
48499
Ha = 221
056 n
mi
Hp = 210
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5563730
88 X = -1666035
58
Y = -15273282
57 feet Y = -4674094
12 meter
Z = 15123448
30 Z = 4601460
62
XDOT = 23221
434559 XDOT = 7059
083435
YDOT = 1148
007641 feet/sec YDOT = 428
956692 meter/sec
ZDOT = 9705
688218 ZDOT = 2992
632799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16175446
79 X = 4930276
18
Y = -1893842
10 feet Y = -577243
07 meter
Z = 15090236
37 Z = 4599504
05
XDOT = -6717
591535 XDOT = -2047
521900
YDOT = 21057
870358 feet/sec YDOT = 6418
438885 meter/sec
ZDOT = 9846
906204 ZDOT = 3001
337011
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12153
07369884
00016717 00000-0 10270-3 0 9150
2 25544 51
6381 202
9942 0010393 11
8035 348
3360 15
55858305 15501
Satellite: ISS
Catalog Number: 25544
Epoch time: 12153
07369884 = yrday
fracday
Element set: 915
Inclination: 51
6381 deg
RA of node: 202
9942 deg
Eccentricity:
0010393
Arg of perigee: 11
8035 deg
Mean anomaly: 348
3360 deg
Mean motion: 15
55858305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 305
Coasting Arc #17 (Orbit 1564)
---------------------------------------
Vector Time (GMT): 2012/154/00:29:01
963
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -717603
79 A = 6772247
14 meter
Y = 4183548
44 meter E =
0020551
Z = -5292777
30 I = 51
50962
XDOT = -7404
954329 Wp = 57
77607
YDOT = -1891
667568 meter/sec RA = 197
20413 deg
ZDOT = -481
896243 TA = 207
55797
MA = 207
66707
Ha = 221
009 n
mi
Hp = 209
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2354343
15 X = -738620
15
Y = 13725552
63 feet Y = 4175406
84 meter
Z = -17364754
93 Z = -5296314
04
XDOT = -24294
469582 XDOT = -7380
909971
YDOT = -6206
258426 feet/sec YDOT = -1974
339857 meter/sec
ZDOT = -1581
024420 ZDOT = -517
811664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12898211
20 X = -3931374
77
Y = -5201196
51 feet Y = -1585324
70 meter
Z = -17379647
39 Z = -5297316
52
XDOT = 10997
516729 XDOT = 3352
043099
YDOT = -21393
703361 feet/sec YDOT = -6520
800784 meter/sec
ZDOT = -1728
615691 ZDOT = -526
882063
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12154
03713384
00016717 00000-0 10270-3 0 9166
2 25544 51
6368 198
1775 0010360 14
6084 345
5368 15
55919097 15654
Satellite: ISS
Catalog Number: 25544
Epoch time: 12154
03713384 = yrday
fracday
Element set: 916
Inclination: 51
6368 deg
RA of node: 198
1775 deg
Eccentricity:
0010360
Arg of perigee: 14
6084 deg
Mean anomaly: 345
5368 deg
Mean motion: 15
55919097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1565
Checksum: 324
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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